A proof of local existence of the problem for supersonic flow past a three-dimensional wing

zbMATH Open0695.76028MaRDI QIDQ910306

Shuxing Chen

Publication date: 1990

Published in: Chinese Science Bulletin (Search for Journal in Brave)

zbMATH Keywords

supersonic flowattached shock frontboundary value problem of nonlinear hyperbolic systemfixed characteristic boundarywing with a small attack angle

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Transonic flows (76H05)

Related Items (1)

On the existence of self-similar solutions in the supercritical region on a delta wing in a hypersonic flow

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